|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
hydromechanical control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:France
|
|
gptkbp:designated_as
|
gptkb:SNECMA
|
|
gptkbp:diameter
|
approximately 1.1 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 3
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Spey
two
Astazou family
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
twin-spool turbofan
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:first_flight
|
gptkb:1955
gptkb:1980s
|
|
gptkbp:fuel_economy
|
0.78 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Astazou engine
|
|
gptkbp:length
|
approximately 3.5 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:SNECMA
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_users
|
gptkb:Air_France
|
|
gptkbp:operational_range
|
up to 30,000 ft
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
not equipped
approximately 5,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Caravelle_family
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:service_entry
|
gptkb:1956
|
|
gptkbp:startup_method
|
air start
|
|
gptkbp:successor
|
gptkb:SNECMA_M53
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Sud_Aviation_SE_210_Caravelle
|
|
gptkbp:weight
|
approximately 1,200 lb
|
|
gptkbp:year_established
|
gptkb:1955
|
|
gptkbp:bfsParent
|
gptkb:Turbomeca
|
|
gptkbp:bfsLayer
|
6
|